To quote ARP themselves:
"The process begins right at the mill, where ARP orders
only premium grade materials including several proprietary
alloys. The ever-popular 8740 chrome moly steel, for
example, comes from the mill in four distinct grades. The
lowest is “commercial,” which is followed by “aircraft quality.”
ARP uses only the top two grades (SDF and CHQ), which
cost twice as much, but provide the foundation for defect-free
fasteners. These materials come in bar stock (for studs) and
huge coils (for bolts).
Transforming raw material into a fastener begins with
“hot” and “cold” heading processes. Material is fed into powerful
devices and cold forged, or induction-heated and formed under tons of pressure.
Following the basic shaping, material is heat-treated to
desired levels. This crucial process is done entirely in-house
to assure total quality control. ARP uses special vertical racks
to hold each piece individually and assure complete 360° penetration.
This is far superior to commonly-used methods of
dumping items into a large bin and batch-treating.
Studs are centerless ground to guarantee concentricity.
The thread rolling operation (to MIL-S-8879A specs) is done
after heat-treat, which accounts for a fatigue strength up to
ten times higher than fasteners which are threaded prior to
heat-treat.
ARP manufactures nuts in a multi-step process that begins
with raw material being fed into a giant forming device that
“blanks” the hex and 12-point nuts and continues with highly
sophisticated automated threading equipment tapping each
nut with an accuracy of .001˝ (which is five times higher than
the aerospace standard). This ensures an exceptionally close tolerance
fit between the bolt/stud and nut.
Metal finishing is also performed in-house at ARP.
Operations include black oxide coating of chrome moly or polishing stainless steel to a brilliant lustre.
Some of the tests that ARP personnel perform on an ongoing
basis include proof loading (using a 120,000 lb. capability tensile
machine), fatigue cycle (Amsler) and hardness (Rockwell).
Visual inspections include use of an Optical Comparator (to
check thread root contour, etc.), fixtured micrometers and
microscopic grain flow analysis. The computer-controlled
fatigue cycle testers allow ARP to take fasteners to a failure
point in millions of cycles – as opposed to the aerospace norm
of 65,000 average to 130,000 cycles maximum. This allows
ARP engineers to verify the design specifications of each
fastener, and prove its ability to provide superior long-term
service."
And yes, I do sell them and have used them personally...